Online Books by
Richard R. Cullom
Books from the extended shelves:
- Cullom, Richard R.: Altitude test of several afterburner configurations on a turbofan engine with a hydrogen heater to simulate an elevated turbine discharge temperature (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Roy L. Johnsen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Cullom, Richard R.: Experimental investigation of a 90 degree flat plate magnetic triode for direct energy conversion (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Cullom, Richard R.: Experimental investigation of the feasibility of ablation-cooling a rocket nozzle with possible application to solid-propellant engines (National Aeronautics and Space Administration, 1961), also by Lewis Research Center (page images at HathiTrust)
- Cullom, Richard R.: Full-scale altitude engine test of a turbofan exhaust-gas-forced mixer to reduce thrust specific fuel consumption (National Aeronautics and Space Administration ;, 1977), also by Roy L. Johnsen and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Cullom, Richard R.: Operating condition and geometry effects on low-frequency afterburner combustion instability in a turbofan at altitude (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Roy L. Johnsen, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Cullom, Richard R.: Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor (National Aeronautics and Space Administration, 1959), also by Ralph L. Schacht, Arthur W. Goldstein, and Lewis Research Center (page images at HathiTrust)
- Cullom, Richard R.: Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude (National Aeronautics and Space Administration Scieentific and Technical Information Branch ;, 1983), also by David M. Straight, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
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